The Present Status of Aircraft Stability Problems in the Aeroelastic Domain

Author:

Taylor A. S.

Abstract

In his classic paper, The Expanding Domain of Aeroelasticity, Collar indicated how various types of problems (involving at least two of the three kinds of force—aerodynamic, elastic and inertial), which had hitherto been dealt with in their own “watertight compartments,” were tending to coalesce into a single subject which might be defined as “the dynamics of a deformable aeroplane.” The title of the subject, as Collar pointed out, at once suggests (to the mathematician at least) the formal solution of the problems which it comprises.

Publisher

Cambridge University Press (CUP)

Reference22 articles.

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2. Dobson A. M. (1956). The Response of the Wing and Engines of the Viscount 700 Series to a Vertical Gust Vickers-Armstrongs (Aircraft) Ltd. Report VTO/700/108, ARC 18,974, June 1956.

3. Brown S. C. and Holleman E. C. (1956). Experimental and Predicted Lateral-Directional Dynamic-Response Characteristics of a Large Flexible 35° Swept-Wing Airplane at an Altitude of 35,000 ft. N.A.C.A. T.N. 3874, December 1956.

4. Harper R. P. Jr. (1955). Flight Evaluations of Various Longitudinal Handling Qualities in a Variable Stability Jet Fighter. Wright Air Development Center Technical Report 55-299, July 1955. (M.O.S. P.57724.)

5. Cole H. A. , Brown S. C. and Holleman E. C. (1954). Experimental and Predicted Longitudinal Response Characteristics of a Large Flexible 35° Swept-Wing Airplane at an Altitude of 35,000 ft. N.A.C.A. Research Memo RM A54H09, N.A.C.A./T.I.L. 5103, November 1954.

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